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Home , Dextre, Expedition 16, Spacelab, Takao Doi

Revision T, PCN-2 August 2009 MISSIONS SUMMARY Page 190 - STS-123/1JA

LANDING SITE/ SSME-TL CREW LAUNCH SITE, RUNWAY, NOM-ABORT SRB ORBIT PAYLOAD MISSION HIGHLIGHTS (6+1 UP/6+1 DN) FLT ORBITER LIFTOFF TIME, CROSSRANGE EMERG RSRM FSW WEIGHTS, (LAUNCH SCRUBS/DELAYS, NO. LANDING SITES, LANDING THROTTLE AND INC HA/HP PAYLOADS/ TAL WEATHER, ASCENT I-LOADS, TITLE, NAMES ABORT TIMES TIMES PROFILE ET EXPERIMENTS FIRSTS, SIGNIFICANT ANOMALIES, ETC.) & EVA'S FLT DURATION, ENG. S.N. WINDS Revision T, PCN-2 August 2009 SPACE SHUTTLE MISSIONS SUMMARY Page 190 - STS-123/1JA STS- 0V-105 CDR: KSC 39A KSC 15 (KSC 104/104/10 BI-133 51.6 DIRECT OI- CARGO: BRIEF MISSION SUMMARY: STS-123/1JA 123/ (Flight 21) Dominic L. Gorie 071:06:28:14Z 68) 9% (25) INSERTION 32 38915 LBS (25th ISS mission) delivered the first ISS ENDEAVO (Flt 4 - STS-91, STS- 2:28:14 AM EDT 087:00:39:06Z RSRM (3) pressurized component of the Japanese UR 99, STS-108) (P) 8:39:06 PM 101 POST OMS- PAYLOAD Kibo Laboratory to ISS, delivered a 1JA 2:28:14 AM EDT EDT PREDICTED: 2: CHARGEABLE: 100/104.5/1 Canadian robotic device called , and OMS P756/R242/V157/M2 (A) Wednesday ET-126 124.9X84.8 30762 LBS provided five spacewalks. Endeavour’s SEQ 11 Tuesday (17) (16) 04.5/72/104. NM PODS: 5 16-day flight was the longest shuttle FLT #122 LPO3-32 3/11/08 (9) 03/26/08 (9) SLWT DEPLOYED: mission to the ISS. The Japanese PLT: 30 29442 LBS RPO4-28 LAUNCH DEORBIT Experiment Logistics Module Pressurized FRC5-21 Gregory H. Johnson ACTUAL: Section (ELMPS or JLP), the smaller of two KSC-122 P757/R322/M278 WINDOW: BURN: NON- 4M54S 086:23:33:13.9 100/104.5/9 DEPLOYED: pressurized modules of Kibo, was attached 9/ MS 1/EV2: (PLT IN-PLANE) Z ET 1132 LBS temporarily to a docking port on the PAD 39A- Robert L. Behnken 72/104.5 IMPACT DEORBIT: space-facing side of Harmony. Kibo, which 45 P758/R323/M279 EOM PLS: KSC XRANGE:187.7 : HA 190.0 MIDDECK: means “hope,” is the major Japanese TAL: ZZA NM 1 = 2047 NM 188 LBS (JAXA) contribution to the Station, and will TAL WX: BEN MET HP 22.5 MLP-3 MS 2/EV3: (11) increase its research capability in a variety Michael J. Foreman ORBIT DIR: A/R 1:14:05 NM SHUTTLE of disciplines. The Dextre is SELECTED: (14) 2 = 2044 ACCUMULATE P759/R324/M280 (10) designed somewhat like the human form 25TH RTLS: KSC 15 LAT: ENTRY D WEIGHTS: with a torso, a head area (camera), and SHUTTLE MS 3: N/N AIM PT: 3 = 2054 (7) 36.723 VELOCITY: arm appendages. It rides on the SSRMS as FLIGHT , JAXA TAL: ZZA 30L NOMINAL S 25859 FPS DEPLOYED: a “dexterous tool for ORU changeout TO ISS (Flt 2 - STS-87) N/N 1423027 LBS without requiring a space walk.” This (MRN: NO-GO) MLGTD: 2174 M 3 EOM: LONG: ENTRY AOA: NOR 23 FT WEIGHT: 158.95 RANGE: NON- mission included representation of all five P760/R231/V195/M2 N/N 087:00:39:06Z 208629.5 7W 4402 NM DEPLOYED: Station partner interests - the U.S., Japan, 01 1ST DAY PLS: VEL: 202 KGS LBS 1601668 LBS , Russia, and the (ESA). EDW 04 N/N 200 KEAS X CG: MS 4/EV1: HDOT: -1.8 FPS CARGO TOTAL: Richard M. Linnehan TDEL: 1080.57 IN 3901248 LBS KSC W/D: OPF: 159, VAB HB-1: 7, PAD A: 23 = (Flt 4 - STS-78, STS- 189 Total Work Days (+ 14 holidays @ OPF) 90, STS-109) 0.000 (P) -0.288 TD NORM 195: (A) 2707 FT LANDING: PERFORMANC WEIGHT: E MARGINS LAUNCH POSTPONEMENTS: P760/R214/V150/M18 MAX Q NAV: DRAG CHUTE: (LBS): 208762 LBS - Added STS-123 to FDRD - launch date of NET 7 754.38 (P) DEPLOY: 192 FPR: 2651 12/08/07 on 11/14/06 758.53 (A) KEAS X CG: FUEL BIAS: MS 5 UP/EV4/EXP - Postponed to 02/14/08 on 04/16/07. Slip due to 087:00:39:10Z 1081.8 IN 1063 STS-117 rollback 16/17 FLT ENG: SRB STG: NLGTD: 5351 FINAL TDDP: Garrett E. Reisman - Postponed to 03/11/08 on 01/28/08. Slip due 2:05.44 (P) FT 2109 to ECO sensor problems experienced during P761/R325/M281 2:04.64 (A) 087:00:39:16Z RECON: 5128 VEL: 161 KGS December launch attempt of STS-122 MS 5 DN/EXP 16 FLT PERF: NOMINAL 158 KEAS PAYLOADS: ENG: HDOT: -4.6 FPS LAUNCH SCRUBS: None Leopold Eyharts, 2 ENG TAL PLB: ESA (ZZA): BRK INIT: 57 ISS-1JA (JAXA LAUNCH WINDOW: (UP on STS-122, 2:39 (P)2:41 (A) KGS LOGISTICS Total launch window was 9 minutes 44 seconds Stay on ISS. Also MODULE) with window open at 071:06:23:20Z and close at flew on Feb NEG RETURN: DRAG CHUTE 071:06:33:04Z. Preferred Launch Time was 1998.) 3:54 3:55 JETTISON: 58 MIDDECK: 071:06:28:14Z (In-Plane Time) for a launch P762/R321/M277 KGS ISS-1JA window of 4m54s. PTA (U/S 158 087:00:39:55Z FPS): 5 CRYO TANK Chief Steve Lindsey flying the Shuttle 5:046 5:016 BRK DECEL SETS Training Aircraft said, “It’s a really nice night out SS EVA 117 FPS 2 : DOCKED QUEST EVA here.” PAO: “Florida’s east coast is about to get SE TAL (ZZA AVE 2.7 PK 4.1 RMS (79) an early sunrise!” 40 104): EMU/TETHERED EVA 5:57 6:04 WHEELS STOP: ODS 110 087:00:40:36Z OBSS LAUNCH DELAYS: None. Launch occurred on SCHEDULED EVA 108 PTM (U/S 181 13629 FT STS123-S-009 (11 March SSPTS time at 2:28 a.m. EDT, Tuesday, March 11, 2008. DURATION 7:01 FPS): 2008) --- Overcast clouds at An eclipse of the GOES-East weather satellite 6:05 6:03 ROLLOUT: 6500 ft provided a spectacular prevented using any satellite imagery in the SSA EVA 118 11455 FT night image as the clouds hour prior to launch. Fortunately, the low clouds DOCKED QUEST EVA SE PRESS 104: 1:30 M:S remained well behaved as skies were cloudy but 41 6:56 6:57 glowed from the Shuttle’s above the range safety and Return to Launch EMU/TETHERED EVA Site (RTLS) cloud ceiling limits. 111 SCHEDULED EVA 109 Continued… Continued… DURATION 7:09 Continued… Continued… Revision T, PCN-2 August 2009 SPACE SHUTTLE MISSIONS SUMMARY Page 191 - STS-123/1JA LANDING SITE/ SSME-TL CREW LAUNCH SITE, RUNWAY, NOM-ABORT SRB ORBIT PAYLOAD MISSION HIGHLIGHTS (6+1 UP/6+1 DN) FLT ORBITER LIFTOFF TIME, CROSSRANGE EMERG RSRM FSW WEIGHTS, (LAUNCH SCRUBS/DELAYS, NO. LANDING SITES, LANDING THROTTLE AND INC HA/HP PAYLOADS/ TAL WEATHER, ASCENT I-LOADS, TITLE, NAMES ABORT TIMES TIMES PROFILE ET EXPERIMENTS FIRSTS, SIGNIFICANT ANOMALIES, ETC.) & EVA'S FLT DURATION, ENG. S.N. WINDS Revision T, PCN-2 August 2009 SPACE SHUTTLE MISSIONS SUMMARY Page 191 - STS-123/1JA STS- Continued… Continued… Continued… Continued… 123/ ISS 1JA SS EVA 119 MECO CMD: WINDS: TAL WEATHER: DOCKED QUEST EVA 8:23.6 8:22.6 1.5T 1.3L KTS Weather at the TAL sites was tricky as showers Continued 42 OFFICIAL: were monitored near Zaragoza, Spain and Istres, … EMU/TETHERED EVA VI: 01002P03 KTS France during the launch countdown. Post cold 112 25819 25817.6 2H 2R KTS front low level wind flow from the northwest SCHEDULED EVA 110 brought showers to the windward sides of the DURATION 6:47 OMS-2: DENS ALT:-336 38:15 38:30 FT Pyrenees and central French mountains. These 97.4 FPS 96.1 showers dissipated as they crossed the high SS EVA 120 terrain. TAL weather was GO. DOCKED QUEST EVA FPS FLT DURATION: 43 15:18:10:52 EMU/TETHERED EVA PERFORMANCE ENHANCEMENTS: 113 S/T: Include the standard set plus: 1) PE Operational SCHEDULED EVA 111 1153:00:57:10 High Q WIN/MAR, 2) OMS Assist, 3) A 52 nm DURATION 6:24 MECO, and 4) Del Psi OV-105: SS EVA 121 235:02:18:33 FLIGHT DURATION CHANGES/LANDING: DOCKED QUEST EVA Deorbit burn was planned for 086:21:58:14Z. 44 DISTANCE: Due to low clouds moving in at KSC, the deorbit EMU/TETHERED EVA 6,577,857 sm burn was delayed to second opportunity at 114 086:23:33:13.9Z. Landing occurred at SCHEDULED EVA 112 TOTAL 087:00:39:06Z, Wednesday, 03/26/08, at DURATION 6:02 SHUTTLE DISTANCE: 8:39:06 PM EDT. 467,923,507 sm FIRSTS/LASTS: - First 16-day Assembly Mission, MCC WHITE FCR (52) 12 days docked. (Longest mission is STS-67 - FLIGHT DIRECTORS: , 16D 21H 47M 35S.) SHUTTLE: - Tied the current mission record of five ASC - B. C. Lunney spacewalks held by the HST Servicing Missions LD/O1 - M. P. Moses (STS-61, STS-82, and STS-109). Most EVA’s O2 - R. E. LaBrode docked to ISS. PLNG - M. R. Abbott - A redesign to RSRM Nozzle Joints 2 and 5, the ENT - R. S. Jones latter with an additional bolt enhancement, MOD - P. L. Engelauf follows up the new Nozzle-to-Case J-leg Joint Team 4 - R. S. Jones/ insulation configuration that debuted on STS- A. J. 122’s motors. Ceccacci - First flight of a lighting system derived from an off-the-shelf flash (Nikon SB800) was added to ISS: a digital camera (in orbiter umbilical well) to LD/O2 - D. J. Weigel capture photos of ET after separation for about O1 - K. L. Alibaruho O 3 - G. Kerrick 130 ft away. Team 4 - H. L. Rarick - This is the last modified tank (before Columbia) IP FD - E. J. Nelson and the next will be a tank built with all mods (I/F w/CSA & JAXA) done in line. - First on-orbit test of orbiter tile repair CAPCOMS: technique. SHUTTLE: ISS016-E-032598 (12 March 2008) --- The Canadian-built Dextre - First time the OBSS was left on the Station so A/E - J. P. Dutton robotic system and the Japanese Kibo laboratory (JLP) are visible that the next flight can deliver the large JAXA K. A. Ford (Wx) Kibo module. LD/O1 - T. W. Virts in Endeavour's cargo bay on approach to ISS. - This mission marks a significant milestone with O2 - N. J. Patrick the inauguration of the JAXA IP support to real- PLNG - B. A. Drew time operations, adding them to the fold with Team 4 - N/A ESA, CSA, and Russia. “We have reached a new pinnacle in the ‘international’ part of the Continued… Space Station operations.” - Spacelab Logistics Pallet (SLP) used by Dextre made its fourth and final flight to space, “concluding a long history that can be traced back before the first shuttle left the launch pad.” - PAO. - First flight with John Shannon as Shuttle Program Manager. NOTE: The unmanned cargo ship Jules Verne, the ESA’s first Automated Transfer Vehicle (ATV), launched toward ISS on March 7. It was parked well away from ISS at a safe distance Revision T, PCN-2 August 2009 SPACE SHUTTLE MISSIONS SUMMARY Page 191 - STS-123/1JA Revision T, PCN-2 August 2009 SPACE SHUTTLE MISSIONS SUMMARY Page 192 - STS-123/1JA LANDING SITE/ SSME-TL CREW LAUNCH SITE, RUNWAY, NOM-ABORT SRB ORBIT PAYLOAD MISSION HIGHLIGHTS (6+1 UP/6+1 DN) FLT ORBITER LIFTOFF TIME, CROSSRANGE EMERG RSRM FSW WEIGHTS, (LAUNCH SCRUBS/DELAYS, NO. LANDING SITES, LANDING THROTTLE AND INC HA/HP PAYLOADS/ TAL WEATHER, ASCENT I-LOADS, TITLE, NAMES ABORT TIMES TIMES PROFILE ET EXPERIMENTS FIRSTS, SIGNIFICANT ANOMALIES, ETC.) & EVA'S FLT DURATION, ENG. S.N. WINDS Revision T, PCN-2 August 2009 SPACE SHUTTLE MISSIONS SUMMARY Page 192 - STS-123/1JA STS- Continued… Continued… 123/ ISS ISS: NIGHT LAUNCH #30: Shannon: “We are O1 - Z. Jones launching in the dark.” 1JA LD/O2 - S. K. Continue Robinson NIGHT LANDING KSC #16: (#22 in Shuttle d… O3 - M. T. Vande Hei history) Team 4 - R. C. Dempsey RENDEZVOUS #70: Rendezvous and dock with ISS EVENTS: - OMS2 ignition at 071:07:06:44.0Z resulted in a 124.9 by 84.8 nm orbit. - SRMS OBSS/LDRI survey of nosecap and port and starboard wing RCC (WLE’s) was completed. - TI maneuver at 073:00:42:21.9Z resulted in a 186.3 by 180.6 nm orbit. - R-Bar Pitch Maneuver was performed. No issues - Docking contact occurred at 073:03:46:54Z. - Hard Dock occurred at 073:04:02:11Z - ISS Hatch opened at 073:05:36:00Z, 12:36 AM CDT, Thursday, March 13, 2008, ISS crew welcoming - IELK Seat Liner Transfer at 073:07:50Z (2:50 AM CDT, March 13, 2008). At that time Leopold Eyharts/ESA became a member of STS-123 and joined the ISS Expedition 16/17 as Flight Engineer. - The first transfer item after hatch opening was swapping Garrett Reisman/MS for Leopold Eyharts (ESA)/Expedition 16 FE. The transfer was official when the form-fitting seatliners were swapped. Eyharts spent 33 days as a member of ISS Expedition 16. With S123-E-007088 (18 March 2008) --- Canada’s two armed the on-time landing of March 26, Eyharts spent a total of 48 days in space. robot, Dextre, is shown in the grasp of the station's robotic - FD4/5: EVA 1: EV1 & EV4: JLP prepped for Canadarm2. unberthing, shuttle robot arm grappled JLP, (ORU) and Tool Changeout Mechanism installed on the Canadian Special Purpose Dexterous Manipulator (SPDM or Dextre) arm 2 and arm 1, shuttle arm unberthed JLP, and shuttle arm installed JLP onto Harmony zenith port (temporary location until Kibo delivery on STS- 124). Unable to provide keep-alive power to SPDM (later determined to be flawed cable in pallet). EVA 1 duration 7:01 - FD6: While Expedition 16 and STS-123 crewmembers brought the Kibo logistics module to life, Dextre’s power supply unit was brought to life via the SSRMS. - FD6: EVA 2: EV1 & EV3: EVA ran long due to problems with the SPDM Arm Expandable Diameter Fasteners (EDF’s) not releasing per procedure. Crew ended up using a pry bar. Time didn’t permit removing some of the SPDM blankets. EV3 experienced RTV delamination. Per Rule {1JA_C2-105}, EMU OVERGLOVE EXCEPTIONS, crew continued the SPDM assembly task without donning overgloves due to the thermal constraints on SPDM. EV3 donned overgloves once the thermal critical tasks were complete. ISS multimeter was repaired and would later be swapped with shuttle multimeter prior to hatch closure. Installed the Node 2/JLP vestibule barrier assembly. EVA 2 duration 7:09 Revision T, PCN-2 August 2009 SPACE SHUTTLE MISSIONS SUMMARY Page 192 - STS-123/1JA Revision T, PCN-2 August 2009 Page 193 - STS-123/1JA SPACE SHUTTLE MISSIONS SUMMARY LANDING SITE/ SSME-TL CREW LAUNCH SITE, RUNWAY, NOM-ABORT SRB ORBIT PAYLOAD MISSION HIGHLIGHTS (6+1 UP/6+1 DN) FLT ORBITER LIFTOFF TIME, CROSSRANGE EMERG RSRM FSW WEIGHTS, (LAUNCH SCRUBS/DELAYS, NO. LANDING SITES, LANDING THROTTLE AND INC HA/HP PAYLOADS/ TAL WEATHER, ASCENT I-LOADS, TITLE, NAMES ABORT TIMES TIMES PROFILE ET EXPERIMENTS FIRSTS, SIGNIFICANT ANOMALIES, ETC.) & EVA'S FLT DURATION, ENG. S.N. WINDS Revision T, PCN-2 August 2009 Page 193 - STS-123/1JA SPACE SHUTTLE MISSIONS SUMMARY STS- Continued… 123/ - FD8: RTV Loss in EVA Gloves: EV3’s gloves ISS were NO-GO for subsequent EVA’s. First spare 1JA set used on EVA 4. Continue - FD8: EVA3: EV1 & EV2: Finished assembly of d… Dextre, including installation of tool holder assembly and a Camera Light Pan Tilt Assembly (CLPA) which serves as Dextre’s eyes. Also, the Spacelab Logistics Pallet used for assembly was prepared for return to shuttle cargo bay. Attempted to install MISSE-6 experiment (unsuccessful - moved to EVA5). EVA 3 duration 6:53 - FD10: Japanese Prime Minister called to congratulate the crew. - FD10: During press interview, asked to describe the fast-growing Space Station, Reisman said the crew was struck by the view SIGNIFICANT ANOMALIES: during final approach and similarities with the Orbiter: famous Space Station scene in the movie -Sensor Unit S/N 1150 on the port wing had “2001: A Space Odyssey” by Stanley Kubrick excessive triggers (quantity 4452) during the and Arthur C. Clarke. Clarke died during this first hour of MMOD monitoring for Late mission on 3/19/08 at the age of 90. Clarke in Inspection. “First on the Moon” stated, “The inspirational -Integrated Sensor Inspection System Sensor value of the space program is probably of far Pack 1 Pan Tilt Unit 10 degrees offset greater importance to education than any S123-E-009262 (24 March 2008) --- The ISS latest configuration is -DCS OI1 card 1 failure input of dollars…a whole generation is growing viewed from Endeavour post-separation. -FES shutdown on Primary A Controller up which has been attracted to the hard -GG Chamber pressure indicated a shift upward disciplines of science and engineering by the -APU 1 fuel tank pressure decay romance of space.” -LH OMS Pod mid surface temperature - FD11: EVA4: EV2 & EV3: Tasks were Remote -Sensor Unit 1150 (Ref Des: 65V08A01) on the Power Control Module removal and port wing replacement, and the Tile Repair Ablator -APU 3 seal cavity drain line pressures indicate Dispenser (T-RAD) detailed test objective slow decay. worksite setup and demonstration. The -Body Flap tile damage demonstration was considered a “huge” -Aft arrowhead damage success, but needs results from post-landing -STBD FWD RAD Retract Flexhose did not fully detailed analysis. EVA 4 duration 6:24 retract into RRSC (ref SPC# 205181853). - FD13: EVA 5: EV2 & EV3: Primary tasks -APU 1 Gas Generator Chamber Pressure completed were positioning of OBSS to Transducer shift temporary home on ISS truss, installation of -Cabin Temp Controller 1 noisy MISSE-6 experiment, and inspection of SARJ. -MPS E-3 LOX Inlet pressure showed a shift of 30 EVA 5 duration 6:02 psi at Liftoff. - FD14: Conducted Rigidizable Inflatable Gas -MADS PCM MSRMNT gradually and abruptly Experiment (RIGEX) funded by the Air Force. moved to OSH throughout the MADS and RIGEX was designed to test how well ground MMU1/SSR1 recording phase. models and computer simulations predict what -Lost OMS POD (RH OMS024) putty repair happens to the inflated structures in -Damage to the V070-391044-174 (BRI-18) tile weightlessness. Once rigid, the sample tubes -Damage to the V070-191101-043 (BRI-18) tile aboard Endeavour were blasted with vibrations SRB: to test their structural integrity. The -Loss of data from SRB RH ET Observation experiment was returned to Earth aboard the Camera during Ascent shuttle for further scientific analysis. RSRM: None - Transfers: SSME: None ● Hardware transferred to Station (outside and ET: None inside: 25839 lbs MOD: ● Hardware transferred to Station (outside): -White-VTS-Servers hung 23776 lbs Integration: ● Hardware transferred to Station (inside): -Unexpected debris/expected debris exceeding 1432 lbs ● Japanese pressurized logistics module: 18377 lbs ● Dextre - Special Purpose Dexterous Manipulator: 3431 lbs ● Middeck items returned from ISS aboard Endeavour: 1565 lbs ● Water transferred to Station: 608 lbs ● Oxygen transferred to Station: N/A ● Nitrogen transferred to Station: 23 lbs - Undocked at 085:00:25:00Z followed by a Revision T, PCN-2 August 2009 Page 193 - STS-123/1JA SPACE SHUTTLE MISSIONS SUMMARY